Douglas DC-8-73F

Service difficulty reports · 15,471

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC873F'
  ORDER BY difficulty_date DESC"

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SDR UPS97824446Bulkhead Angle · crackedINSPECTION TYPE-C, FOUND RT MLG W/W UPPER BULKHEAD ATTACH ANGLE CRACKED FS 861, BL 47 RT. REMOVED CRACKED ATTACH ANGLE, FABRICATED NEW ATTACH ANGLE, DRILLED, TREATED, PRIME AND INSTALLED IAW DC8 SRM 53-1-0, 51-1-21, 51-1-8, 51-1-20D.Sep 4, 1997 · N808UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS97824445Clip · corrodedINSPECTION TYPE-C, FOUND CORROSION ON LONGERON 31 RT, FS 35 BEHIND ATTACH CLIP ON FRAME. REMOVED ATTACH CLIP, REMOVED CORROSION FROM FRAME IAW DC8 SRM 51-1-8, FABRICATED NEW ATTACH CLIPS, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-20D, 53-2-0.Sep 4, 1997 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97824425Fitting · corrodedINSPECTION TYPE-D, C-3 DOOR AFT TORQUE BOX SUPPORT FITTING AT FS 1228 BTWN LONG 32R AND 33R HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 AND 51-01-20.Sep 4, 1997 · N809UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97824373Skin · crackedDURING C-CHECK INSPECTION, FOUND LT WING LEAKING EDGE CRACKED AT STA XFS 198, 29 FWD OF UPPER WING FRONT SPAR. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW UPS EO DC8-5720-7767-A AND DC8 SRM 51-1-21 AND 51-1-8.Sep 4, 1997 · N808UP · Doug DC873F · Wing, Plate/SkinSDR DHL9780716CVane · delaminatedAT C-CHECK, LT O/B FLAP I/B VANE ASSY HAS DELAMINATION. REMOVED, SENT FOR REPAIR AND REINSTALED PER MM 27-51-14.Sep 4, 1997 · N807DH · Doug DC873F · Trailing Edge FlapsSDR DHL9780714CVane · delaminatedAT C-CHECK, RT WING T/E O/B VANE DELAMINATED. REMOVED AND REPAIRED PER MM 27-51-14.Sep 4, 1997 · N807DH · Doug DC873F · Trailing Edge FlapsSDR DHL9780711CBracket · crackedAT C-CHECK, LT MLG WHEEL WELL UPPER FWD SECTION BRACKET CRACKED. REMOVED BRACKET AND FABRICATED AND INSTALLED PER SRM 51-1-20D.Sep 4, 1997 · N807DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9780709CDoor · delaminatedAT C-CHECK, RT MLG CENTER DOOR TEMPORARY REPAIR DELAMINATED. REPAIRED DOOR PER SRM 51-3-2.Sep 4, 1997 · N807DH · Doug DC873F · Landing Gear DoorsSDR DHL9780708CDoor · delaminatedAT C-CHECK, LT MAIN OUTBD DOOR DELAMINATED, REMOVED DOOR, OVERHAULED AND REINSTALLED PER MM 32-12-1.Sep 4, 1997 · N807DH · Doug DC873F · Landing Gear DoorsSDR DHL9780706CSpar · bulgedAT C-CHECK, LT UPPER T/E REAR SPAR XRS 172.00 HAS BULGE IN T/E PANEL. REMOVED REPAIR, INSPECTED AREA, NO CORROSION AND REINSTALLED REPAIR PER SRM 51-1-21.Sep 4, 1997 · N807DH · Doug DC873F · Wing SparSDR DHL9780705CTab · dentedAT C-CHECK, RT ELEVATOR CONTROL TAB HAS DENT. REMOVED AND REPLACED TAB PER MM 27-30-2.Sep 4, 1997 · N807DH · Doug DC873F · Elevator, Tab StructureSDR UPS97824654Skin · crackedINSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND 2 CRACKS ON LT WING AT XRS90 BETWEEN CENTER SPAR AND STRINGER 9. REMOVED DAMAGED AREAS, FABRICATED REPAIR DOUBLER AND FILLERS, DRILLED, TREATED, PRIMED AND INSTALLED DOUBLER AND FILLERS IAW DC8 SRM 57-2-1 FIGSep 3, 1997 · N808UP · Doug DC873F · Wing, Plate/SkinSDR UPS97824648Fitting · crackedINSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND RE MLG TORQUE TUBE SUPPORT FITTING CRACKED AT F/S 902 AND 878. REMOVED MLG TORQUE TUBE SUPPORT FITTING, FITTED NEW TORQUE TUBE SUPPORT FITTING, DRILLED, TREATED AND INSTALLED IAW UPS E.O. DC8-5340-0748-F.Sep 3, 1997 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97824632Skin · corrodedINSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND AREAS'S OF EXTERNAL SKIN BULGING AND RIVETS PULLING THROUGH SKIN F/S 1620 TO 1690 LONGERON 31 RT TO 31 LT. REMOVED SKIN FROM F/S 1480 TO 1690, REMOVED CORROSION FROM AREA, DRILLED, TREATED, PRIMED AND INSTALLSep 3, 1997 · N808UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS97824569Panel · crackedINSPECTION TYPE-N/A, FOUND LT WING UPPER INBD SLOT PANEL CRACKED .75 LONG AT STA XFS220. REMOVED CRACKED SLOT PANEL, DRILLED, TREATED, PRIMED AND INSTALLED NEW SLOT PANEL IAW DC8 SRM 57-1-0, 51-1-8, 51-3-0, 51-1-21.Sep 3, 1997 · N808UP · Doug DC873F · Trailing Edge FlapsSDR UPS97824568Rib · crackedINSPECTION TYPE-N/A, FOUND RT WING INBD FLAP OTBD RIB (END CAP) CRACKED AT LOWER ANGLE STA XW138. REMOVED CRACKED END CAP, FABRICATED NEW END CAP, DRILLED, TREATED, PRIMED AND INSTALLED END CAP IAW DC8 SRM 57-1-0, 51-1-8, 51-1-21, 51-3-0.Sep 3, 1997 · N808UP · Doug DC873F · Trailing Edge FlapsSDR UPS97824558Angle · crackedINSPECTION TYPE-C, FOUND RT WING INBD FLAP AFT LOWER ATTACH ANGLE CRACKED AT OTBD RIB STA XW 138. REMOVED CRACKED ATTACH ANGLE, FABRICATED NEW ATTACH ANGLE, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-21 AND DACO DWG 5652396.Sep 3, 1997 · N808UP · Doug DC873F · Trailing Edge FlapsSDR UPS97824557Angle · crackedINSPECTION TYPE-C, FOUND RT WING INBD FLAP LOWER ATTACH ANGLE CRACKED AT OTBD RIB STA XW 138. REMOVED CRACKED ATTACH ANGLE, FABRICATED NEW ATTACH ANGLE, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 57-1-0, 51-1-8, 51-1-21.Sep 3, 1997 · N808UP · Doug DC873F · Trailing Edge FlapsSDR UPS97824556Angle · crackedINSPECTION TYPE-C, FOUND LT WING INBD SLOT PANEL, OTBD SPLICE PAN ANGLE CRACKED AT AFT END, STA XW 223. REMOVED CRACKED PAN ANGLE, DRILLED, TREATED, PRIMED AND INSTALL NEW PAN ANGLE IAW DC8 SRM 57-1-0, 51-1-8, 51-1-21.Sep 3, 1997 · N808UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS97824553Fitting · crackedINSPECTION TYPE-C, FOUND ATTACH FITTING AT STA 880 ABOVE LONGERON 24 RT. REMOVED CRACKED FITTING, LOCATED AND DRILLED NEW FITTING, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-1-0, 51-1-8, 51-3-0, 51-1-20D.Sep 3, 1997 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97824444Angle · crackedINSPECTION TYPE-C, FOUND LT WING INBD FLAP OTBD LOWER INTERCONNECT PANEL ATTACH ANGLE CRACKED AT AFT END STA XW138. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, DRILLED, TREATED, PRIMED AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0, 51-1-20D, 51-1-8.Sep 3, 1997 · N808UP · Doug DC873F · Wing Miscellaneous StructureSDR DHL9780707CSkin · damagedAT C-CHECK, LT WING OUTBOARD FLAP TEMP REPAIR ON LOWER SURFACE. REMOVED REPAIR AND CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS PER SRM 57-2-5 FIG. 1Sep 3, 1997 · N807DH · Doug DC873F · Trailing Edge FlapsSDR DHL9780704CPanel · delaminatedAT C CHECK, RT FLAP SCISSOR PANEL HAS DELAMINATED INNER UPPER AREA. REMOVED PANEL, REPAIRED, AND INSTALLED PANEL PER MM 27-50-0.Sep 3, 1997 · N807DH · Doug DC873F · Trailing Edge FlapsSDR DHL9780703CAntenna · delaminatedAT C CHECK, LEFT LOWER ADF SENSE ANTENNA NR 162S DELAMINATED. REMOVED AND REPLACED ANTENNA PER MM 34-30-0.Sep 3, 1997 · N807DH · Doug DC873F · Automatic Direction Finder (ADF) SystemSDR DHL9780702CPanel · delaminatedAT C CHECK, RT PANEL NR 162P HAS CORROSION AND SKIN BULGE. PANEL REMOVED AND REPAIRED AND REINSTALLED PER M/M 20-35-1.Sep 3, 1997 · N807DH · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS97824372Floor Track · wornDURING C-CHECK INSPECTION, FOUND FLOOR TRACK TANG OUT OF LIMITS COMPT 17 BL 24 LT STA 1485. REMOVED DAMAGED SECTION OF TRACK, DRILLED, TREATED, PRIMED, AND INSTALLED TRACK PLUG IAW DC8 SRM 53-2-3 FIG 6D, 51-1-8, 51-3-0.Sep 2, 1997 · N808UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS97824371Floor Track · wornDURING C-CHECK INSPECTION, FOUND FLOOR TRACK TANGS OUT OF LIMITS ON PREVIOUS PLUG REPAIR COMPT 4 BL 45 LT FS 560. REMOVED DAMAGED PLUG, DRILLED, TREATED, PRIMED AND INSTALLED NEW PLUG IN TRACK IAW DC8 SRM 53-2-3 FIG 6 D, 51-1-8, 51-3-0.Sep 2, 1997 · N808UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9780701CPanel · delaminatedAT C CHECK, LEFT WING AT STA XW5.00 PANEL DELAMINATED. REMOVED AND REPAIRED PANEL AND REINSTALLED PER SRM 51-3-0.Sep 2, 1997 · N807DH · Doug DC873F · Wing, Plate/SkinSDR SRAA970901Actuator · out of adjustON LANDING AT IST FOR FLIGHT 248, SPOILERS DID NOT DEPLOY AUTOMATICALLY, MANUALLY DEPLOYED SPOILERS. OPS CHECKED GROUND SHIFT MECHANISM, FOUND ACTUATOR OUT OF RIG, RERIGGED SYSTEM FOR CORRECT SPOILER DEPLOYMENT PER MM CH 27-60.Aug 28, 1997 · N873SJ · Doug DC873F · Drag Control ActuatorSDR DHL97805005Relay · malfunctionedWHEN THRUST LEVERS ADVANCED, AND FLAPS RETRACTED TO 0, THE TAKEOFF CONFIGURATION HORN CAME ON. REPLACED NR 1 MISC GROUND CONT RELAY, OPS CHECKED GOOD .Aug 26, 1997 · N805DH · Doug DC873F · Central WarningSDR DHL97805004Temp Sensor Wire · brokenAFTER TAKEOFF NOTICED STRONG VIBRATOIN WITH BOTH PACKS ON. TURNING LEFT PACK OFF ALLEVIATED THE PROBLEM. FOUND BROKEN WIRE AT 35 DEGREE TEMP SENSOR.Aug 26, 1997 · N805DH · Doug DC873F · Cabin Temperature SensorSDR RRXA97241Oxy Regulator · out of positionLOSS OF O2 PRESS, DURING FLT. FOUND FIRST OBSERVERS O2 REGULATOR IN EMERGENCY. PLACED IN NORMAL, SERVICED O2 TO PROPER LIMITS. NO LEAKS NOTED.Aug 25, 1997 · N870TV · Doug DC873F · Crew Oxygen SystemSDR UPS97824320Web · crackedINSPECTION TYPE-D, FS 50 TO 130 RBL 44 FLOOR WEB CORRODED AND CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM 51-1-20D, 51-1-21, AND DWG 9753289.Aug 24, 1997 · N809UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97824332Bracket · crackedINSPECTION TYPE-D, LT ELEV CONTROL TAB MOUNT 2ND FROM INBD IS CRACKED. REMOVED AND REPLACED BRACKET ASSY IAW SRM 51-1-21.Aug 23, 1997 · N809UP · Doug DC873F · Elevator StructureSDR UPS97824451Floorbeam · crackedINSPECTION TYPE:D N/R/C 620816 WRITTEN TO REMOVE FLOOR PANELS FROM FS 980 TO 1540 FOR ADDITIONAL INSPECTION OF FLOORBEAMS, DUE TO EXCESSIVE CORROSION IN AREA. FLOORBEAM CORRODED AND CRACKED FS 1500 LBL 48. REPAIRED FLOORBEAM IAW DHC SK-809-900.Aug 20, 1997 · N809UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS97824342Floorbeam · corrosionINSPECTION TYPE-D, FS 1180 LBL 24 FLOORBEAM CORROSION BEYOND LIMITS. REPAIRED IAW DHC SK-809-891.Aug 20, 1997 · N809UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS97824293Angle · crackedDURING C CHECK INSPECTION, FOUND ATTACH ANGLE CRACKED F/S 640 BETWEEN LONGERON 26 AND 27 RT. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE, DRILLED, PRIMED AND INSTALLED NEW ANGLE IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D, 51-1-21Aug 19, 1997 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97824261Fitting · crackedDURING C-CHECK INSPECTION, FOUND FITTING CRACKED AT LONG 36 FS 350. REMOVED CRACKED FITTING, CUT NEW FITTING, FABRICATED SPLICES, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0 FIG 2D, 51-1-8, 51-1-20D.Aug 18, 1997 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97824260Angle · crackedDURING C-CHECK INSPECTION, FOUND ATTACH ANGLE CRACKED FS 640 BETWEEN LONGERON 26 AND 27 LT. REMOVED CRACKED ANGLE, FABRICATED NEW REPAIR ANGLE IAW DC8 SRM 53-2-0, TREATED, PRIMED AND INSTALLED REPAIR ANGLE IAW DC8 SRM 51-1-8, 51-1-21, 51-1-20D AND 53-2-0.Aug 18, 1997 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97824292Skin · crackedDURING C CHECK INSPECTION, FOUND TWO CRACKS AT EDGE OF FLAP SKIN OTBD OF EXHAUST GATE LT WING APPROX STA XRS 325. STOP DRILLED CRACKS, FABRICATED REPAIR DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 57-2-1 FIG 20 PG 25, 51-1-8, 51-1-21.Aug 17, 1997 · N811UP · Doug DC873F · Trailing Edge FlapsSDR UPS97824291Stiffener · crackedDURING C CHECK INSPECTION, FOUND STIFFENER CRACKED OUTBOARD SIDE OF RT MAIN WHEEL WELL FWD OF FLAP DRUM AT STA 940. REMOVED CRACKED STIFFENER, FABRICATED NEW STIFFENER, DRILLED, TREAT, PRIMED AND INSTALLED NEW STIFFENER IAW DC8 SRM 53-2-0, 51-1-21.Aug 17, 1997 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97824258Fitting · crackedDURING C-CHECK INSPECTION, FOUND FRAME FITTING CRACKED AND CORRODED FS 940 ABOVE LONGERON 24 RT. REMOVED DAMAGED FITTING, CUT NEW FITTING, DRILLED NEW FITTING, SPLICES AND INSTALLED IAW DC8 SRM 53-2-0 FIG 8, 51-1-8, 51-1-21, 51-1-20D.Aug 17, 1997 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS97824251Angle · corrodedDURING C-CHECK INSPECTION, FOUND FLOOR SUPPORT BEAM ATTACH ANGLE CORRODED STA 781.5 AT BL 68 LT. REMOVED FLOOR SUPPORT BEAM LOWER ATTACH ANGLE, DRILLED NEW ATTACH ANGLE AND INSTALLED IAW DC8 SRM 53-2-0 PG 1 PAR 3, 51-1-20, 51-1-8.Aug 17, 1997 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA97222Retract Mech · out of adjustAFTER TAKEOFF, THE CREW ON N604AL HEARD A LOUD NOISE IN THE NOSE GEAR. CREW ELECTED TO RETURN TO SJO. ACFT LANDED WITHOUT INCIDENT. AFTER INSPECTION, NO PROBLEM COULD BE FOUND. CREW ATTEMPED TO TAKEOFF AGAIN, BUT PERFORMED AN AIR TURNBACK WITH SAME PROBLEAug 17, 1997 · N604AL · Doug DC873F · Landing Gear Retraction/Extension SystemSDR UPS97824290Fitting · crackedDURING C CHECK INSPECTION, FOUND RT WING OTBD FLAP STA XF 408 (INBD) FLAP HINGE SUPPORT FITTING CRACKED. CRACK IS OUT OF SRM LIMITS. REMOVED SUPPORT FITTING AT STA 408, LOCATED, DRILLED AND INSTALLED NEW SUPPORT FITTING IAW DC8 SRM 57-1-0, 51-3-0.Aug 16, 1997 · N811UP · Doug DC873F · Wing, Control Surface Attach FittingsSDR RRXA97221Floor Heater · defectiveAT CRUISE SMOKE FILLED COCKPIT. SUSPECT FLOOR HEAT RIGHT AFT CAPT'S SEAT. TRANSFERRED TO NON MEL NR 10, FOUND FLOOR HEATER DEFECTIVE. DISCONNECTED HEATER, PULLED C/B'S AND COLLARED. DEACTIVATED FLOOR HEATER PER MA AM-2140-02;00. THIS CLEARS NON MEL NR 10.Aug 14, 1997 · N604AL · Doug DC873F · Heating SystemSDR UPS97824426Skin · corrodedINSPECTION TYPE-D, RT HORZ STAB L/E O/B SECTION CORROSION REMOVAL BETWEEN SKIN OUT OF LIMITS, REF NR 621494. REPAIRED L/E SKIN IAW SRM 55-3-0, 55-2-0, 53-2-0, 55-3-1, AND 51-1-21.Aug 12, 1997 · N809UP · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR UPS97824138Floorbeam · crackedINSPECTION TYPE-C, FS 55 LBL 25 TO 33 FLOORBEAM HAS NUMEROUS HOLES BROKEN OUT ON EDGE OF FLOORBEAM. REPAIRED IAW DHC-SK-868-115.Aug 12, 1997 · N868UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS97824135Angle · crackedINSPECTION TYPE-C, INTERCOSTAL ATTACH ANGLE AT FS 882 RBL 61 CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-20D 53-2-0.Aug 11, 1997 · N868UP · Doug DC873F · Fuselage Miscellaneous StructureSDR SRAA970805Actuator · failedAFTER TAKEOFF OUT OF BRU, FLIGHT 131 - AIRCRAFT LOST ALL HYDRAULIC FLUID, FOUND NR 3 ENGINE HYDRAULIC LOW PRESSURE LIGHT ON, FOLLOWED BY NR 2 ENGINE SYSTEM. FLUID CAME DOWN TO EMERGENCY LEVEL, ACCOMPLISHED AIR TURN BACK TO BRU AFTER DUMPING 19,000 LBS OF FUELAug 10, 1997 · N874SJ · Doug DC873F · Aileron Control System
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